US20040144113A1 - Heat extraction system for cooling power transformer - Google Patents

Heat extraction system for cooling power transformer Download PDF

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Publication number
US20040144113A1
US20040144113A1 US10/351,712 US35171203A US2004144113A1 US 20040144113 A1 US20040144113 A1 US 20040144113A1 US 35171203 A US35171203 A US 35171203A US 2004144113 A1 US2004144113 A1 US 2004144113A1
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Prior art keywords
chillant
heat
heat energy
heat exchanger
refrigeration system
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US10/351,712
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Robert Longardner
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RW Inc
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RW Inc
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Priority to US10/351,712 priority Critical patent/US20040144113A1/en
Assigned to RW, INC. reassignment RW, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LONGARDNER, ROBERT L.
Priority to US10/887,289 priority patent/US20040255604A1/en
Publication of US20040144113A1 publication Critical patent/US20040144113A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B27/00Machines, plants or systems, using particular sources of energy
    • F25B27/02Machines, plants or systems, using particular sources of energy using waste heat, e.g. from internal-combustion engines

Definitions

  • the present invention relates to power transformers, which may be step-up or step-down transformers.
  • the manufacturing of electricity begins at the power plant, where natural gas, oil, coal or other fuels are burned in a boiler producing steam under high pressure and/or in air breathing heat engines (ABHE), which turns a turbine connected to a generator having a large magnet surrounded by coiled copper wire. The turbine causes the magnet to rotate inside the coils and generate electricity by creating a current in each coil.
  • ABHE air breathing heat engines
  • the power is “stepped up” to a very high voltage by a large power transformer for more economical transmission over long distances to different substations.
  • a substation is comprised of electrical apparatus that generally transforms the voltage to lower levels. From the substations the power then travels to other distribution transformers. These transformers again reduce the voltage to the 120-volt and 240-volt levels required for appliances and equipment.
  • the power is channeled to distribution panels and home circuit breakers. It is at this point that the power is divided up into several circuits that serve different loads.
  • transformers are highly efficient and can deliver practically the full power received in the primary coil to the secondary coil.
  • transformer losses typically in the form of heat, can reduce transformer efficiency, resulting in a reduction of load that the transformer can serve.
  • Examples of transformer losses affected by heat and load which can be metered are: copper loss, hyteresis loss, eddy current loss, iron loss, no-load loss, and impedance loss.
  • heat from transformer losses can degrade the insulation of the transformer, leading to reduced life of the transformer.
  • the invention provides a system and method for improving the inner workings of a power transformer and simultaneously conditioning the intake air to an air breathing heat engine (ABHE) as taught in U.S. Pat. No. 4,936,109 of the present inventor.
  • ABHE air breathing heat engine
  • the inventive system also may modulate the heat from losses described herein and provide for the ‘on-line’ conditioning of the heat from a power transformer.
  • the system for improving efficiency of power transformers includes a power transformer, a device for dissipating the heat energy, and a refrigeration system that uses the dissipated heat energy to produce a chillant.
  • the chillant is then re-circulated and used to lower the temperature of the power transformer system.
  • the device for dissipating the heat energy may be a liquid to liquid heat exchanger or a liquid to air heat exchanger.
  • the refrigeration system may be an absorption chiller that employs heat energy to produce a chillant by energizing a staged process of concentration, condensation, evaporation and absorption of a mixture of gas and liquid.
  • the system may further include a gas compressor that generates heat energy during gas compression, and a device for recovering the heat energy to supply to the refrigeration system producing a chillate.
  • the device for recovering heat energy may include a post-compression heat exchanger.
  • the chillant from the refrigeration system is used in a heat exchange process to condition the intake air to the compressor.
  • the gas compressor may further include a pre-compression heat exchanger, which also receives the chillant from the refrigeration system and an embodiment to provide chillant for reducing the heat related transformer losses.
  • the pre-compression heat exchanger serves to cool the intake gas prior to the compression process, so that the energy used for gas compression can be reduced.
  • the system of the present invention further includes an air breathing heat engine (ABHE) operably coupled to the gas compressor, whereby the gas compressor compresses air that flows through the ABHE.
  • the compressed air is mixed with fuel, and ignited to create a combustion force to run the ABHE.
  • exhaust gas containing heat energy is produced.
  • the ABHE has a device for recovering the heat energy from the exhaust gas.
  • the device may be a post-combustion heat exchanger located downstream of the combustion area. The heat exchanger recovers heat energy from the exhaust gas by a heat exchange process. The recovered heat energy is then transferred to the refrigeration system for use in the production of chillant.
  • the post-combustion heat exchanger is embodied to provide heat energy that can produce chillant from the refrigeration system to use in the heat exchange process.
  • the ABHE may be connected, by a shaft, to a generator for power generation.
  • the combustion force generated in the ABHE is used to drive the shaft, which in turn drives the generator.
  • the system of the present invention includes a steam turbine, instead of the ABHE.
  • the steam turbine receives pressurized steam from a steam source, such as a boiler. Once entering the steam turbine, the pressurized steam expands with an output of power that can drive a shaft to actuate a connected power generator. After complete expansion, the steam flows into a downstream condenser to be condensed and cooled. The steam changes to hot water carrying heat energy that can be transferred to the refrigeration system. The refrigeration system can use this additional heat energy for the production of chillant.
  • the steam turbine may provide hot water to a connected hot water heater, which distributes hot water for various purposes.
  • One advantage of the invention is that it provides the method for cooling the inner working of a transformer for all atmospheric and load conditions while other directed chillate is conditioning the ambient air stream to the ABHE which magnifies the amount of electrical energy for retail by 20-30% when ambient termperatures are around 95° F. (35° C.) compared to the through-put for turbine ISO or transformer nameplate rating.
  • the chillate provides the means to protect the transformer against the damage of temperature rise due to the heat gain in the inherent losses.
  • FIG. 1 is a diagram showing an embodiment of the system of the present invention
  • FIG. 2 is a graph depicting rising transformer temperature and showing a zone in which chilled oil is used to augment ambient cooling;
  • FIG. 3 is a diagram of another embodiment of the present invention, showing the heat generating section
  • FIG. 4 is a diagram of an alternative embodiment of the present invention, showing the heat generating section.
  • system 10 for improving a power transformer efficiency generally includes power transformer 20 generating heat through transformation losses such as heat due to resistance flow of current, heat due to hysteresis, heat due to eddy currents, and heat due to no-load.
  • the efficiency of transformer 10 can be calculated in terms of energy units (kilowatt hour, Kwh):
  • Power transformer 20 may be any commercially available transformer, such as any one of the common classes of transformers listed in TABLE 1.
  • TABLE 1 The most common classes of transformer THE MOST COMMON CLASSES OF TRANSFORMER CLASS COOLING METHOD OA OUTSIDE-AIR SELF-COOLED (BY CONVECTION) OA/FA OUTSIDE-AIR/FAN-AIR SELF-COOLED OR FAN COOLED OA/FA/FA OUTSIDE-AIR W/2 FAN SELF-COOLED/FAN COOLED COOLING SETS OA/FA/FOA OUTSIDE-AIR/FAN-AIR/FORCED (PUMPED) OIL SELF-COOLED, FAN COOLED PUMPED OIL FOA FORCED OIL/FAN COOLED PUMPED OIL WITH FANS AA AIR-AIR DRY TYPE (OR CAST INSULATION) SELF COOLED (BY CONVECTION) AA/FA AIR-
  • Transformer 20 may have transformer coil (not shown) that is made of any suitable material such as copper wire.
  • transformer coil (not shown) that is made of any suitable material such as copper wire.
  • Power transformer 20 may have various built-in overload capabilities, and existing cooling method as shown in TABLE 1.
  • the existing cooling method requires a supply of external energy.
  • a cooling fan requires a connection to an outside electrical source.
  • the existing cooling method may be replaced or complemented by system 10 of the present invention.
  • System 10 further includes device for dissipating heat energy 30 in communication with power transformer 20 .
  • device for dissipating heat energy 30 includes heat exchanger 31 .
  • Heat exchanger 31 may include elongated tube 29 defining interior space 32 and hollow coil 33 disposed within interior space 32 and extending from inlet connection 41 along the length of tube 29 to outlet connection 40 .
  • Medium line 24 has first end 34 connected to power transformer 20 , and second end 35 open into interior space 32 at first end 36 of tube 29 .
  • First end 34 of first medium line 24 is connected to power transformer 20 through valve 50 , which can open when the internal temperature of power transformer 20 reaches a predetermined temperature, and can close as the internal temperature of power transformer 20 drops below the predetermined temperature.
  • Medium return line 25 has a first end 43 open into interior space 32 at second end 37 of tube 29 , and second end 44 in communication with power transformer 20 .
  • First chillant line 52 and first chillant return line 53 are in communication with heat exchanger 31 and refrigeration system 60 .
  • First chillant line 52 has first end 55 connected to and in communication with refrigeration system 60 , and second end 54 connected to and in communication with hollow coil 33 at inlet connection 41 of tube 29 .
  • First chillant return line 53 has first end 57 connected to and in communication with hollow coil 33 at outlet connection 40 of tube 29 , and second end 56 connected to and in communication with refrigeration system 60 .
  • Refrigeration system 60 may include any suitable absorption chiller or refrigeration generator available in the market. Examples of absorption chillers and refrigeration generators that can be used in system 10 are described in U.S. Pat. No. 4,936,109, the disclosure of which is herein fully incorporated by reference. Generally, an absorption chiller or a refrigeration generator employs heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide a chillant for cooling purposes. The chillant may be in a fluid form, such as water or gas.
  • refrigeration system 60 produces chillant 62 that is transferred through first chillant line 52 into hollow coil 33 at inlet connection 41 of heat exchanger 31 .
  • medium 21 which may be an oil, water, a gas, or any other cooling fluid that circulates inside power transformer 20 .
  • Medium 21 becomes heated medium 22 as the temperature rises.
  • valve 50 opens to release heated medium 22 into medium line 24 .
  • the ambient temperature may affect the temperature of medium 21 , but will not influence the operation of valve 50 .
  • Heated medium 22 from medium line 24 enters interior space 32 of tube 29 at first end 36 . While in tube 29 , heat energy is transferred to chillant 62 in hollow coil 33 by a heat transfer process, resulting in cool medium 21 , and heated chillant 64 .
  • the initial temperature of chillant 62 may be about 50° F. (10° C.). After the heat transfer process, the temperature of heated chillant 64 may reach a about 80° F. (29.4° C.).
  • Cool medium 21 exits tube 29 from second end 37 and enters medium return line 25 to travel back to power transformer 20 . Cool medium 21 circulates inside power transformer 20 to capture additional heat energy released from power transformer 20 . Simultaneously, heat energy captured in heated chillant 64 is transferred to refrigeration system 60 to energize a staged process of concentration, condensation, evaporation and absorption to produce chillant 62 having a sufficiently cool temperature.
  • system 70 further includes gas compressor 72 , and post-compression heat exchanger 80 positioned downstream of gas compression area 75 within gas compressor 72 .
  • Post-compression heat exchanger 80 may include sensible cooling coil 78 which receives chillant 62 from refrigeration system 60 .
  • Sensible cooling coil 78 extends within compressor 72 .
  • chillant 62 becomes heated chillant 64 , which is transferred back to refrigeration system 60 .
  • Refrigeration system 60 uses the heat energy in the staged process of concentration, condensation, evaporation, and absorption to produce another chillant 62 , as described hereinabove.
  • System 70 further includes second chillant line 82 , and second chillant return line 83 .
  • Second chillant line 82 is connected to and in communication with refrigerator system 60 and post-compression heat exchanger 80 .
  • Second chillant line 82 may have a first end 84 branching from first chillant line 52 .
  • First end 84 and first chillant line 52 may form a T-position 85 , allowing chillant 62 produced by refrigeration system 60 to move in two directions, one within first chillant line 52 toward heat exchanger 31 (see FIGS. 1 and 3), another within second chillant line 83 toward post-compression heat exchanger 80 .
  • Second end 88 of chillant line 82 connects to first end 89 of sensible cooling coil 78 .
  • Second chillant return line 83 is connected to and in communication with post-compression heat exchanger 80 and refrigeration system 60 , allowing heated chillant 64 to be transferred from post-compression heat exchanger 80 to refrigeration system 60 .
  • Second chillant return line 83 has first end 90 connected to second end 92 of sensible cooling coil 78 .
  • Second end 91 of second chillant return line 83 may form a T-position 86 with first chillant return line 53 .
  • Heated chillant 64 from first chillant return line 53 and second chillant return line 83 combine at T position 86 before moving along chillant return line 53 toward refrigeration system 60 .
  • first end 84 of second chillant line 82 may be in direct communication with refrigeration system 60 , without first joining first chillant line 52 .
  • second end 91 of second chillant return line 83 may be in direct communication with refrigeration system 60 , without first joining first chillant return line 53 .
  • chillant 62 from refrigeration 60 will be transferred through a separate second chillant line 82 all the way to post-compression heat exchanger 80 .
  • heated chillant 64 from post-compression heat exchanger 80 will be transferred through a separate second chillant return line 83 all the way to refrigeration system 60 .
  • system 70 may include pre-compression heat exchanger 71 positioned within compressor 72 upstream of post-compression heat exchanger 80 for cooling the gas that enters compressor 72 prior to or at the same time as gas compression. Lowering the temperature of the gas, prior to or simultaneously with the gas compression, reduces the energy required to compress the gas.
  • Heat exchanger 71 may include air condition coil 74 in communication with second chillant line 82 through extension line 94 , and second chillant return line 83 through extension line 95 .
  • Air condition coil 74 receives chillant 62 from refrigeration system 60 through second chillant line 82 and extension line 94 , and returns heated chillant 64 to refrigeration system 60 through extension line 95 and second chillant return line 83 .
  • compressor 72 may be driven by any power engine, such as a steam turbine engine, an electric motor, internal combustion engine. Air supplied through gas intake 73 flows through pre-compression heat exchanger 71 , whereby heat energy in the air is transferred by a heat exchange process into chillant 62 contained in air condition coil 74 . The air is compressed in compressor 72 , releasing heat energy. The compressed air then passes post-compression heat exchanger 80 , and through compressed gas line 76 to a place where the compressed air is to be used or stored. Post-compression heat exchanger 80 recovers heat energy by a process of heat exchange, wherein heat energy is transferred to chillant 62 in sensible cooling coil 78 , producing heated chillant 64 .
  • any power engine such as a steam turbine engine, an electric motor, internal combustion engine.
  • Air supplied through gas intake 73 flows through pre-compression heat exchanger 71 , whereby heat energy in the air is transferred by a heat exchange process into chillant 62 contained in air condition coil 74 .
  • the air is compressed in compressor 72
  • Heated chillant 64 from pre-compression heat exchanger 71 combined with that from post-compression heat exchanger 80 is transferred to refrigeration system 60 , which uses the combined heat energy to produce chillant 62 , in the same way as what described herein above.
  • Chillant 62 is circulated back to air condition coil 74 and sensible cooling coil 78 .
  • chillant 62 has a temperature of 42° F. (5.6° C.) when it is supplied to sensible cooling coil 78 and air condition coil 74
  • heated chillant 64 may have a temperature of 52° F. (11° C.) when heated chillant 64 returns to refrigeration system 60 .
  • system 70 further includes air breathing heat engine (ABHE) 100 .
  • air breathing heat engine 100 includes combustor 101 and turbine 102 which utilizes combustion force from combustor 101 to drive shaft 103 .
  • Shaft 103 is drivingly connected to a generator 106 for power generation.
  • Air breathing heat engine 100 is positioned downstream of compressed gas line 76 .
  • Compressed air from compressor 72 is mixed with injected fuel in combustor 101 and the air and fuel mixture is ignited resulting in a combustion force that drives shaft 103 to actuate generator 106 .
  • Exhaust gas 107 is produced as a result of the combustion is ported via conduit 108 to a waste heat recovery unit 111 , having combustion heat exchanger 112 positioned within flue 117 of heat recovery unit 111 .
  • Combustion heat exchanger 112 includes at least one chillant coil 113 receiving chillant 62 from refrigeration system 60 .
  • combustion heat exchanger 112 includes top chillant coil 114 stacked above bottom chillant coil 115 . Both top chillant coil 114 and bottom chillant coil 115 are connected to and in communication with chillant supply line 116 and chillant return line 118 .
  • air breathing heat engine 100 may further include an acoustic enclosure, as described in U.S. Pat. No. 6,082,094, the disclosure of which is herein incorporated by reference.
  • Refrigeration 60 may supply chillant 62 for ventilating the acoustic enclosure via appropriate chillant supply line connection (not shown) or through an additional heat exchanger placed within the acoustic enclosure, or as described in U.S. Pat. No. 6,082,094.
  • refrigeration system 60 of system 10 and 70 may simultaneously receive heat energy from power transformer 20 , compressor 72 , and air breathing heat engine 100 , and use the combined heat energy to generate chillant 62 .
  • Chillant 62 may be supplied to one or more heat exchangers for various cooling purposes as described above.
  • system 120 includes steam turbine 121 connected to and in communication with refrigeration 60 .
  • Refrigeration system 60 is connected to power transformer 20 in the same fashion, as shown in FIG. 1.
  • steam turbine 121 releases heat energy which is transferred to refrigeration system 60 for use in the production of chillant 62 , similar to what discussed hereinabove.
  • Steam turbine 121 may be any known steam turbine that has a suitable configuration.
  • steam turbine 121 includes steam condenser 122 in communication with turbine engine 123 .
  • Turbine engine 123 includes shaft 125 connected to power generator 126 , or other machine or equipment that is operable using power from an engine.
  • Steam turbine 121 receives condensed steam from a source, which can be a boiler of a compatible capacity. The condensed steam enters steam turbine 121 through steam inlet pipe 128 and expands in turbine engine 123 , with an output of power driving shaft 125 to actuate power generator 126 .
  • the expanded steam flows to steam condenser 122 from turbine engine 123 through an appropriate exhaust steam casing (not shown), and is condensed to hot water. Expanded steam or hot water can be returned to the steam source or the boiler through return pipe 129 . Some excess hot water 130 containing heat energy which may be at a temperature of about 210° F. (98.9° C.), may flow through first hot water pipe 132 from condenser 122 to refrigeration system 60 . Refrigeration system 60 uses the heat energy for the production of chillant 62 for cooling power transformer 20 (see FIG. 1).
  • Additional hot water or working fluid 133 may flow through second hot water pipe 134 to hot water heater 140 , which is connected to steam turbine 121 . It is also possible to have excess steam from turbine engine 123 to flow through steam pipe 136 to supply heat to hot water heater 140 .
  • Hot water or working fluid 141 which is a residual hot water derived from hot water 130 flowing through refrigeration system 60 , wherein a portion of heat is extracted from hot water 130 for the production of chillant 62 , may be supplied to hot water heater 140 through third hot water pipe 142 .
  • Output hot water 150 from hot water heater 140 can be distributed for various heating purposes.
  • condenser 122 may contain a heat exchanger that can capture heat energy from condensing the steam. The captured heat energy can then be transferred to refrigeration system 60 , similar to what have been discussed above as relating to gas compressor 72 .
  • both steam turbine 121 and air breathing heat engine 100 are components of the same system. Both turbine 121 and air breathing heat engine 100 may produce heat energy that together can be supplied to refrigeration system 60 . In addition, if air breathing heat engine 100 produces excess heat, the heat energy may be used to heat the water in the connected hot water heater 140 . For particular applications and circumstances, the amount of generated heat apportioned to refrigeration system and hot water heater 140 may be adjusted.
  • Refrigeration system 60 takes advantage of heat energy that is released from internal sources within the system, and minimizes external energy requirements.

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Abstract

The present invention provides systems and methods for improving efficiency of power transformers by capturing heat energy that is produced by air breathing heat engine (ABHE) or a feed water heater to produce chillant. The systems of the present invention may be used with step-down or step-up power transformers. A heat energy dissipation device is in communication with the transformer and may recover heat energy from the ABHE and transformer. A refrigeration system is coupled to the dissipation device to use recovered heat energy to produce chillant which is supplied to the transformer and ABHE. The system may also include a gas compressor and post-compression and pre-compression heat exchangers; steam turbine engines, and power generators.

Description

    BACKGROUND OF THE INVENTION
  • 1. Field of the Invention. [0001]
  • The present invention relates to power transformers, which may be step-up or step-down transformers. [0002]
  • 2. Description of the Related Art [0003]
  • The manufacturing of electricity begins at the power plant, where natural gas, oil, coal or other fuels are burned in a boiler producing steam under high pressure and/or in air breathing heat engines (ABHE), which turns a turbine connected to a generator having a large magnet surrounded by coiled copper wire. The turbine causes the magnet to rotate inside the coils and generate electricity by creating a current in each coil. [0004]
  • From the generator, the power is “stepped up” to a very high voltage by a large power transformer for more economical transmission over long distances to different substations. A substation is comprised of electrical apparatus that generally transforms the voltage to lower levels. From the substations the power then travels to other distribution transformers. These transformers again reduce the voltage to the 120-volt and 240-volt levels required for appliances and equipment. [0005]
  • From the distribution transformers, the power is channeled to distribution panels and home circuit breakers. It is at this point that the power is divided up into several circuits that serve different loads. [0006]
  • Generally, transformers are highly efficient and can deliver practically the full power received in the primary coil to the secondary coil. However, transformer losses, typically in the form of heat, can reduce transformer efficiency, resulting in a reduction of load that the transformer can serve. Examples of transformer losses affected by heat and load which can be metered are: copper loss, hyteresis loss, eddy current loss, iron loss, no-load loss, and impedance loss. In addition, heat from transformer losses can degrade the insulation of the transformer, leading to reduced life of the transformer. [0007]
  • It is prudent to manage transformer losses to prevent overheating. Known systems address the overheat problem of power transformer by using fans or other cooling mechanisms such as cooling oil baths or electric refrigeration systems. Traditionally, the fans or the electric refrigeration systems utilize external sources of energy, therefore, they are not very efficient. [0008]
  • Further improvements in power transformer systems are needed. [0009]
  • SUMMARY OF THE INVENTION
  • The invention provides a system and method for improving the inner workings of a power transformer and simultaneously conditioning the intake air to an air breathing heat engine (ABHE) as taught in U.S. Pat. No. 4,936,109 of the present inventor. The inventive system also may modulate the heat from losses described herein and provide for the ‘on-line’ conditioning of the heat from a power transformer. [0010]
  • In one embodiment of the present invention, the system for improving efficiency of power transformers includes a power transformer, a device for dissipating the heat energy, and a refrigeration system that uses the dissipated heat energy to produce a chillant. The chillant is then re-circulated and used to lower the temperature of the power transformer system. The device for dissipating the heat energy may be a liquid to liquid heat exchanger or a liquid to air heat exchanger. The refrigeration system may be an absorption chiller that employs heat energy to produce a chillant by energizing a staged process of concentration, condensation, evaporation and absorption of a mixture of gas and liquid. [0011]
  • In another embodiment, the system may further include a gas compressor that generates heat energy during gas compression, and a device for recovering the heat energy to supply to the refrigeration system producing a chillate. The device for recovering heat energy may include a post-compression heat exchanger. The chillant from the refrigeration system is used in a heat exchange process to condition the intake air to the compressor. In this particular embodiment, the gas compressor may further include a pre-compression heat exchanger, which also receives the chillant from the refrigeration system and an embodiment to provide chillant for reducing the heat related transformer losses. The pre-compression heat exchanger serves to cool the intake gas prior to the compression process, so that the energy used for gas compression can be reduced. [0012]
  • In yet another embodiment, the system of the present invention further includes an air breathing heat engine (ABHE) operably coupled to the gas compressor, whereby the gas compressor compresses air that flows through the ABHE. The compressed air is mixed with fuel, and ignited to create a combustion force to run the ABHE. At the same time, exhaust gas containing heat energy is produced. The ABHE has a device for recovering the heat energy from the exhaust gas. The device may be a post-combustion heat exchanger located downstream of the combustion area. The heat exchanger recovers heat energy from the exhaust gas by a heat exchange process. The recovered heat energy is then transferred to the refrigeration system for use in the production of chillant. The post-combustion heat exchanger is embodied to provide heat energy that can produce chillant from the refrigeration system to use in the heat exchange process. In a specific embodiment of the present invention, the ABHE may be connected, by a shaft, to a generator for power generation. The combustion force generated in the ABHE is used to drive the shaft, which in turn drives the generator. [0013]
  • In an alternative embodiment, the system of the present invention includes a steam turbine, instead of the ABHE. The steam turbine receives pressurized steam from a steam source, such as a boiler. Once entering the steam turbine, the pressurized steam expands with an output of power that can drive a shaft to actuate a connected power generator. After complete expansion, the steam flows into a downstream condenser to be condensed and cooled. The steam changes to hot water carrying heat energy that can be transferred to the refrigeration system. The refrigeration system can use this additional heat energy for the production of chillant. The steam turbine may provide hot water to a connected hot water heater, which distributes hot water for various purposes. [0014]
  • One advantage of the invention is that it provides the method for cooling the inner working of a transformer for all atmospheric and load conditions while other directed chillate is conditioning the ambient air stream to the ABHE which magnifies the amount of electrical energy for retail by 20-30% when ambient termperatures are around 95° F. (35° C.) compared to the through-put for turbine ISO or transformer nameplate rating. The chillate provides the means to protect the transformer against the damage of temperature rise due to the heat gain in the inherent losses.[0015]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The above-mentioned and other features and advantages of this invention, and the manner of attaining them, will become more apparent and the invention itself will be better understood by reference to the following description of embodiments of the invention taken in conjunction with the accompanying drawings, wherein: [0016]
  • FIG. 1 is a diagram showing an embodiment of the system of the present invention; [0017]
  • FIG. 2 is a graph depicting rising transformer temperature and showing a zone in which chilled oil is used to augment ambient cooling; [0018]
  • FIG. 3 is a diagram of another embodiment of the present invention, showing the heat generating section; [0019]
  • FIG. 4 is a diagram of an alternative embodiment of the present invention, showing the heat generating section.[0020]
  • Corresponding reference characters indicate corresponding parts throughout the several views. Although the drawings represent embodiments of the present invention, the drawings are not necessarily to scale and certain features may be exaggerated in order to better illustrate and explain the present invention. The exemplification set out herein illustrates an embodiment of the invention, in one form, and such exemplifications are not to be construed as limiting the scope of the invention in any manner. [0021]
  • DETAILED DESCRIPTION OF THE INVENTION
  • The embodiments disclosed below are not intended to be exhaustive or limit the invention to the precise form disclosed in the following detailed description. Rather, the embodiments are chosen and described so that others skilled in the art may utilize their teachings. [0022]
  • Referring now to FIG. 1, [0023] system 10 for improving a power transformer efficiency generally includes power transformer 20 generating heat through transformation losses such as heat due to resistance flow of current, heat due to hysteresis, heat due to eddy currents, and heat due to no-load. The efficiency of transformer 10 can be calculated in terms of energy units (kilowatt hour, Kwh):
  • Efficiency=Output/Input=Output (Kwh)/[Output (Kwh)+Heat loss (Kwh)]
  • The voltage regulation of [0024] transformer 20 is the percentage change in the output voltage from no-load to full-load. [% Regulation=(no-load voltage−load voltage)×100/load voltage)]. Ideally, there should be no change in the transformer's output voltage from no-load to full-load. In such a case, the voltage regulation is 0%. To get the best performance out of a transformer, it is necessary to have the lowest possible voltage regulation.
  • [0025] Power transformer 20 may be any commercially available transformer, such as any one of the common classes of transformers listed in TABLE 1.
    TABLE 1
    The most common classes of transformer
    THE MOST COMMON CLASSES OF TRANSFORMER
    CLASS COOLING METHOD
    OA OUTSIDE-AIR SELF-COOLED (BY CONVECTION)
    OA/FA OUTSIDE-AIR/FAN-AIR SELF-COOLED OR FAN COOLED
    OA/FA/FA OUTSIDE-AIR W/2 FAN SELF-COOLED/FAN COOLED
    COOLING SETS
    OA/FA/FOA OUTSIDE-AIR/FAN-AIR/FORCED (PUMPED) OIL SELF-COOLED, FAN COOLED PUMPED OIL
    FOA FORCED OIL/FAN COOLED PUMPED OIL WITH FANS
    AA AIR-AIR DRY TYPE (OR CAST INSULATION) SELF COOLED (BY CONVECTION)
    AA/FA AIR-AIR/FAN-AIR IN DRY TYPE SELF-COOLED WITH FANS
  • [0026] Transformer 20 may have transformer coil (not shown) that is made of any suitable material such as copper wire. In an oil cooled transformer where the hot spot temperature changes the heat of the coil, for example from 95° C. to 115° C., the resistance to current flow would be increased by: (115° C.-95° C.=) 20° C.×43%/100° C.=8.3%. The increased resistance produces lower voltage.
  • By the theorem of Similar Triangles, calculations can be made for comparing power and energy lost in transformer due to increase in resistance within the secondary coil. For example (See FIG. 2), by limiting the rise in the oil temperature an average of 126° F. (52° C.) to 221° F. (105°) when ambient temperature is 95° F. (35° C.), and absolute zero is 459° F. (237.2° C.) these losses are reduced by 4.0% when compared to 248° F. (120° C.) hot spot (See calculation below): [0027] R 248 R 221 = 459 + 153 + 95 459 + 126 + 95 = 1.04
    Figure US20040144113A1-20040729-M00001
  • Similarly when ambient is 50° F. (10° C.) and the oil temperature rise is limited to an average 110° .F (43.3° C.), the resistance to current flow is decreased by 14.0% and the current flow could be increased by 14.0% when compared to 248° F. (120° C.) hot spot (See calculation below): [0028] R 248 R 160 = 459 + 153 + 95 459 + 110 + 50 = 1.14
    Figure US20040144113A1-20040729-M00002
  • [0029] Power transformer 20 may have various built-in overload capabilities, and existing cooling method as shown in TABLE 1. The existing cooling method requires a supply of external energy. For example, a cooling fan requires a connection to an outside electrical source. The existing cooling method may be replaced or complemented by system 10 of the present invention.
  • [0030] System 10 further includes device for dissipating heat energy 30 in communication with power transformer 20. According to FIG. 1, device for dissipating heat energy 30 includes heat exchanger 31. Heat exchanger 31 may include elongated tube 29 defining interior space 32 and hollow coil 33 disposed within interior space 32 and extending from inlet connection 41 along the length of tube 29 to outlet connection 40. Medium line 24 has first end 34 connected to power transformer 20, and second end 35 open into interior space 32 at first end 36 of tube 29. First end 34 of first medium line 24 is connected to power transformer 20 through valve 50, which can open when the internal temperature of power transformer 20 reaches a predetermined temperature, and can close as the internal temperature of power transformer 20 drops below the predetermined temperature. Medium return line 25 has a first end 43 open into interior space 32 at second end 37 of tube 29, and second end 44 in communication with power transformer 20.
  • [0031] First chillant line 52 and first chillant return line 53 are in communication with heat exchanger 31 and refrigeration system 60. First chillant line 52 has first end 55 connected to and in communication with refrigeration system 60, and second end 54 connected to and in communication with hollow coil 33 at inlet connection 41 of tube 29. First chillant return line 53 has first end 57 connected to and in communication with hollow coil 33 at outlet connection 40 of tube 29, and second end 56 connected to and in communication with refrigeration system 60.
  • [0032] Refrigeration system 60 may include any suitable absorption chiller or refrigeration generator available in the market. Examples of absorption chillers and refrigeration generators that can be used in system 10 are described in U.S. Pat. No. 4,936,109, the disclosure of which is herein fully incorporated by reference. Generally, an absorption chiller or a refrigeration generator employs heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide a chillant for cooling purposes. The chillant may be in a fluid form, such as water or gas.
  • As depicted in FIG. 1, [0033] refrigeration system 60 produces chillant 62 that is transferred through first chillant line 52 into hollow coil 33 at inlet connection 41 of heat exchanger 31. At the same time, heat energy from transformer losses is transferred to medium 21, which may be an oil, water, a gas, or any other cooling fluid that circulates inside power transformer 20. Medium 21 becomes heated medium 22 as the temperature rises. When the temperature of heated medium 22 reaches a pre-determined temperature, valve 50 opens to release heated medium 22 into medium line 24. The ambient temperature may affect the temperature of medium 21, but will not influence the operation of valve 50.
  • Heated medium [0034] 22 from medium line 24 enters interior space 32 of tube 29 at first end 36. While in tube 29, heat energy is transferred to chillant 62 in hollow coil 33 by a heat transfer process, resulting in cool medium 21, and heated chillant 64. The initial temperature of chillant 62 may be about 50° F. (10° C.). After the heat transfer process, the temperature of heated chillant 64 may reach a about 80° F. (29.4° C.). Cool medium 21 exits tube 29 from second end 37 and enters medium return line 25 to travel back to power transformer 20. Cool medium 21 circulates inside power transformer 20 to capture additional heat energy released from power transformer 20. Simultaneously, heat energy captured in heated chillant 64 is transferred to refrigeration system 60 to energize a staged process of concentration, condensation, evaporation and absorption to produce chillant 62 having a sufficiently cool temperature.
  • In another embodiment of the present invention, as shown in FIG. 3 in addition to all components of [0035] system 10 in FIG. 1, system 70 further includes gas compressor 72, and post-compression heat exchanger 80 positioned downstream of gas compression area 75 within gas compressor 72. Post-compression heat exchanger 80 may include sensible cooling coil 78 which receives chillant 62 from refrigeration system 60. Sensible cooling coil 78 extends within compressor 72. When gas is compressed, a certain amount of heat energy is released. The heat energy is transferred to chillant 62 within sensible cooling coil 78 by a heat exchange process. As a result, chillant 62 becomes heated chillant 64, which is transferred back to refrigeration system 60. Refrigeration system 60 uses the heat energy in the staged process of concentration, condensation, evaporation, and absorption to produce another chillant 62, as described hereinabove.
  • [0036] System 70 further includes second chillant line 82, and second chillant return line 83. Second chillant line 82 is connected to and in communication with refrigerator system 60 and post-compression heat exchanger 80. Second chillant line 82 may have a first end 84 branching from first chillant line 52. First end 84 and first chillant line 52 may form a T-position 85, allowing chillant 62 produced by refrigeration system 60 to move in two directions, one within first chillant line 52 toward heat exchanger 31 (see FIGS. 1 and 3), another within second chillant line 83 toward post-compression heat exchanger 80. Second end 88 of chillant line 82 connects to first end 89 of sensible cooling coil 78.
  • Second [0037] chillant return line 83 is connected to and in communication with post-compression heat exchanger 80 and refrigeration system 60, allowing heated chillant 64 to be transferred from post-compression heat exchanger 80 to refrigeration system 60. Second chillant return line 83 has first end 90 connected to second end 92 of sensible cooling coil 78. Second end 91 of second chillant return line 83 may form a T-position 86 with first chillant return line 53. Heated chillant 64 from first chillant return line 53 and second chillant return line 83 combine at T position 86 before moving along chillant return line 53 toward refrigeration system 60.
  • In an alternative embodiment (not shown), [0038] first end 84 of second chillant line 82 may be in direct communication with refrigeration system 60, without first joining first chillant line 52. Similarly, second end 91 of second chillant return line 83 may be in direct communication with refrigeration system 60, without first joining first chillant return line 53. In this specific embodiment, chillant 62 from refrigeration 60 will be transferred through a separate second chillant line 82 all the way to post-compression heat exchanger 80. Likewise, heated chillant 64 from post-compression heat exchanger 80 will be transferred through a separate second chillant return line 83 all the way to refrigeration system 60.
  • As further shown in FIG. 3, [0039] system 70 may include pre-compression heat exchanger 71 positioned within compressor 72 upstream of post-compression heat exchanger 80 for cooling the gas that enters compressor 72 prior to or at the same time as gas compression. Lowering the temperature of the gas, prior to or simultaneously with the gas compression, reduces the energy required to compress the gas.
  • [0040] Heat exchanger 71 may include air condition coil 74 in communication with second chillant line 82 through extension line 94, and second chillant return line 83 through extension line 95. Air condition coil 74 receives chillant 62 from refrigeration system 60 through second chillant line 82 and extension line 94, and returns heated chillant 64 to refrigeration system 60 through extension line 95 and second chillant return line 83.
  • In operation, [0041] compressor 72 may be driven by any power engine, such as a steam turbine engine, an electric motor, internal combustion engine. Air supplied through gas intake 73 flows through pre-compression heat exchanger 71, whereby heat energy in the air is transferred by a heat exchange process into chillant 62 contained in air condition coil 74. The air is compressed in compressor 72, releasing heat energy. The compressed air then passes post-compression heat exchanger 80, and through compressed gas line 76 to a place where the compressed air is to be used or stored. Post-compression heat exchanger 80 recovers heat energy by a process of heat exchange, wherein heat energy is transferred to chillant 62 in sensible cooling coil 78, producing heated chillant 64. Heated chillant 64 from pre-compression heat exchanger 71 combined with that from post-compression heat exchanger 80 is transferred to refrigeration system 60, which uses the combined heat energy to produce chillant 62, in the same way as what described herein above. Chillant 62 is circulated back to air condition coil 74 and sensible cooling coil 78. In one example, chillant 62 has a temperature of 42° F. (5.6° C.) when it is supplied to sensible cooling coil 78 and air condition coil 74, whereas, heated chillant 64 may have a temperature of 52° F. (11° C.) when heated chillant 64 returns to refrigeration system 60.
  • In FIG. 3, [0042] system 70 further includes air breathing heat engine (ABHE) 100. As is conventional, air breathing heat engine 100 includes combustor 101 and turbine 102 which utilizes combustion force from combustor 101 to drive shaft 103. Shaft 103 is drivingly connected to a generator 106 for power generation.
  • Air breathing [0043] heat engine 100 is positioned downstream of compressed gas line 76. Compressed air from compressor 72 is mixed with injected fuel in combustor 101 and the air and fuel mixture is ignited resulting in a combustion force that drives shaft 103 to actuate generator 106. Exhaust gas 107 is produced as a result of the combustion is ported via conduit 108 to a waste heat recovery unit 111, having combustion heat exchanger 112 positioned within flue 117 of heat recovery unit 111. Combustion heat exchanger 112 includes at least one chillant coil 113 receiving chillant 62 from refrigeration system 60. As demonstrated in FIG. 3, combustion heat exchanger 112 includes top chillant coil 114 stacked above bottom chillant coil 115. Both top chillant coil 114 and bottom chillant coil 115 are connected to and in communication with chillant supply line 116 and chillant return line 118.
  • In operation, heat energy from [0044] exhaust gas 107 in waste recovery unit 111 is captured in chillant 62 within top chillant coil 114 and bottom chillant coil 115. Chillant 62 becomes heated chillant 64, leaving waste recovery unit 111 through chillant return line 118 to refrigeration system 60. The heat energy is used by refrigeration system 60 to produce chillant 62, as described above. Chillant 62 circulates back to top chillant coil 114 and bottom chillant coil 115 via chillant supply line 116.
  • In a specific embodiment of the present invention (not shown), air [0045] breathing heat engine 100 may further include an acoustic enclosure, as described in U.S. Pat. No. 6,082,094, the disclosure of which is herein incorporated by reference. Refrigeration 60 may supply chillant 62 for ventilating the acoustic enclosure via appropriate chillant supply line connection (not shown) or through an additional heat exchanger placed within the acoustic enclosure, or as described in U.S. Pat. No. 6,082,094.
  • Returning to FIGS. 1 and 3, [0046] refrigeration system 60 of system 10 and 70 may simultaneously receive heat energy from power transformer 20, compressor 72, and air breathing heat engine 100, and use the combined heat energy to generate chillant 62. Chillant 62 may be supplied to one or more heat exchangers for various cooling purposes as described above.
  • In another embodiment shown in FIG. 4, [0047] system 120 includes steam turbine 121 connected to and in communication with refrigeration 60. Refrigeration system 60 is connected to power transformer 20 in the same fashion, as shown in FIG. 1. Generally, steam turbine 121 releases heat energy which is transferred to refrigeration system 60 for use in the production of chillant 62, similar to what discussed hereinabove.
  • [0048] Steam turbine 121 may be any known steam turbine that has a suitable configuration. For example, as depicted in FIG. 4, steam turbine 121 includes steam condenser 122 in communication with turbine engine 123. Turbine engine 123 includes shaft 125 connected to power generator 126, or other machine or equipment that is operable using power from an engine. Steam turbine 121 receives condensed steam from a source, which can be a boiler of a compatible capacity. The condensed steam enters steam turbine 121 through steam inlet pipe 128 and expands in turbine engine 123, with an output of power driving shaft 125 to actuate power generator 126. After complete expansion, the expanded steam flows to steam condenser 122 from turbine engine 123 through an appropriate exhaust steam casing (not shown), and is condensed to hot water. Expanded steam or hot water can be returned to the steam source or the boiler through return pipe 129. Some excess hot water 130 containing heat energy which may be at a temperature of about 210° F. (98.9° C.), may flow through first hot water pipe 132 from condenser 122 to refrigeration system 60. Refrigeration system 60 uses the heat energy for the production of chillant 62 for cooling power transformer 20 (see FIG. 1).
  • Additional hot water or working [0049] fluid 133 may flow through second hot water pipe 134 to hot water heater 140, which is connected to steam turbine 121. It is also possible to have excess steam from turbine engine 123 to flow through steam pipe 136 to supply heat to hot water heater 140.
  • Hot water or working [0050] fluid 141, which is a residual hot water derived from hot water 130 flowing through refrigeration system 60, wherein a portion of heat is extracted from hot water 130 for the production of chillant 62, may be supplied to hot water heater 140 through third hot water pipe 142. Output hot water 150 from hot water heater 140 can be distributed for various heating purposes.
  • In a specific embodiment (not shown), [0051] condenser 122 may contain a heat exchanger that can capture heat energy from condensing the steam. The captured heat energy can then be transferred to refrigeration system 60, similar to what have been discussed above as relating to gas compressor 72.
  • Further, it is possible to combine the embodiments shown in FIGS. 3 and 4, so that both [0052] steam turbine 121 and air breathing heat engine 100 are components of the same system. Both turbine 121 and air breathing heat engine 100 may produce heat energy that together can be supplied to refrigeration system 60. In addition, if air breathing heat engine 100 produces excess heat, the heat energy may be used to heat the water in the connected hot water heater 140. For particular applications and circumstances, the amount of generated heat apportioned to refrigeration system and hot water heater 140 may be adjusted.
  • It is one advantage of the present invention to protect [0053] power transformer 20 by keeping power transformer 20 at a suitable temperature, regardless of the ambient temperature. It is another advantage of the present invention to use one on-line refrigeration system 60 to produce chillant 62 for cooling different components of a power generation system. Refrigeration system 60 takes advantage of heat energy that is released from internal sources within the system, and minimizes external energy requirements.
  • While the present invention has been described as having a preferred design, the present invention can be further modified within the spirit and scope of this disclosure. This application is therefore intended to cover any variations, uses, or adaptations of the invention using its general principles. Further, this application is intended to cover such departures from the present disclosure as come within known or customary practice in the art to which this invention pertains. [0054]

Claims (23)

What is claimed is:
1. A system for improving efficiency of air breathing heat engines (ABHE) and power transformers comprising:
a power transformer;
a heat energy dissipation device in communication with said power transformer and adapted to recover heat energy from the ABHE and said power transformer; and
a refrigeration system operably coupled to said dissipation device using recovered heat energy to produce a chillant, said refrigeration system supplying the chillant to said power transformer and the ABHE.
2. The system of claim 1, wherein said dissipation device includes a transformer heat exchanger.
3. The system of claim 2, wherein said transformer heat exchanger includes a liquid to liquid heat exchanger.
4. The system of claim 2, wherein said transformer heat exchanger includes a liquid to gas heat exchanger.
5. The system of claim 1, wherein said refrigeration system includes an absorption chiller, said chiller employing the recovered heat energy to energize a staged process of concentration, condensation, evaporation and absorption to produce the chillant for cooling said power transformer.
6. The system of claim 1 further comprising:
a gas compressor having a gas compression area; and
a post-compression heat exchanger disposed within said gas compressor, and operably associated with said gas compression area to recover heat energy released when compressed gas is produced by said gas compressor, said post-compression heat exchanger operably coupled with said refrigeration system, said refrigeration system using the recovered heat energy to produce the chillant.
7. The system of claim 6 further comprising:
a pre-compression heat exchanger for cooling pre-compression gas operably coupled with said refrigeration system, said pre-compression heat exchanger utilizing the chillant produced by said refrigeration system for cooling pre-compression gas simultaneously with compression of gas in said gas compressor.
8. The system of claim 6 wherein said refrigeration system includes an absorption chiller, said chiller employing the recovered heat energy to energize a staged process of concentration, condensation, evaporation and absorption to produce the chillant.
9. The system of claim 6 further comprising:
an air breathing heat engine operably coupled to said gas compressor, said air breathing heat engine using the condensed gas from said gas compressor in a combustion to produce heat energy;
a post-combustion heat exchanger operably coupled to said air breathing heat engine and arranged to recover the heat energy produced by said air breathing heat engine, said refrigeration system operably coupled with said post-combustion heat exchanger, said refrigeration system using the recovered heat energy for producing the chillant.
10. The system of claim 9, wherein said air breathing heat engine includes a shaft, and a power generator drivingly connected to said shaft to actuate said power generator.
11. The system of claim 9, wherein said refrigeration system includes an absorption chiller, said chiller employing the recovered heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide the chillant.
12. The system of claim 1 further comprising a steam turbine generating heat energy, said steam turbine connected to and in communication with said refrigeration system, enabling the heat energy to be used by said refrigeration system for producing the chillant.
13. A system for improving a power transformer efficiency which is impacted by heat losses, said system comprising:
a power transformer;
a transformer heat exchanger for dissipating heat energy operably coupled with said power transformer;
a heat generating component generating additional heat energy;
a second heat exchanger for recovering additional heat energy operably coupled with said heat generating component; and
a refrigeration system operably coupled with said transformer heat exchanger and said second heat exchanger, said refrigeration system utilizing the heat energy in a process for producing a chillant, the chillant used for cooling said power transformer.
14. The system of claim 13, wherein said heat generating component is at least one of a gas compressor, an air breathing heat engine (ABHE), and a steam turbine.
15. The system of claim 13, wherein said refrigeration system includes an absorption chiller, said chiller employing the heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide the chillant.
16. The system of claim 13, wherein at least one of said transformer heat exchanger and said second heat exchanger includes a liquid to liquid heat exchanger.
17. The system of claim 13, wherein at least one of said transformer heat exchanger and said second heat exchanger includes a liquid to gas heat exchanger.
18. A method for controlling the internal temperature of a power transformer comprising the steps of:
(a) providing a power transformer unit, a heat exchanger operably coupled with the power transformer, and a refrigeration system operably coupled with the heat exchanger;
(b) dissipating heat energy produced by the power transformer in the heat exchanger;
(c) transferring the heat energy to the refrigeration system;
(d) producing chillant in the refrigeration system using the heat energy; and
(e) transferring the chillant to the power transformer for cooling the power transformer.
19. The method of claim 18 further comprising the steps of:
(f) providing a heat generating component, and a second heat exchanger for recovering additional heat energy produced by the heat generating component;
(g) recovering the additional heat energy in the second heat exchanger;
(h) transferring the additional heat energy to the refrigeration system;
(i) producing additional chillant in the refrigeration system using additional heat energy; and
(j) transferring the additional chillant to the power transformer for cooling the power transformer.
20. The method of claim 19 further comprising the step of:
(k) transferring the additional chillant to the heat generating component for cooling within the heat generating component.
21. The method of claim 19, wherein the heat generating component of said (k) transferring step includes at least one of a gas compressor, an air breathing heat engine (ABHE) and a steam turbine.
22. The method of claim 18, wherein the refrigeration system of said (a) providing step includes an absorption chiller, the chiller employing the recovered heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide the chillant.
23. The method of claim 19, wherein the refrigeration system of said (a) providing step includes an absorption chiller, said chiller employing the recovered heat energy and additional heat energy to energize a staged process of concentration, condensation, evaporation and absorption to provide the chillant.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080178590A1 (en) * 2007-01-29 2008-07-31 General Electric Company Integrated plant cooling system
EP1999766A1 (en) * 2006-03-22 2008-12-10 Seong-Hwang Rim The cooler for transformer using generation cycle
WO2012031791A1 (en) * 2010-09-08 2012-03-15 Siemens Aktiengesellschaft Method and arrangement for drying a transformer component

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3524327A (en) * 1968-05-31 1970-08-18 Air Liquide Method of maintaining electrical apparatus at very low temperatures
US4803958A (en) * 1987-09-08 1989-02-14 Erickson Donald C Absorption heat pumped cogeneration engine
US5581997A (en) * 1993-10-19 1996-12-10 California Energy Commission Performance enhanced gas turbine powerplants
US6321552B1 (en) * 1998-06-22 2001-11-27 Silentor Holding A/S Waste heat recovery system
US6484501B1 (en) * 1998-02-03 2002-11-26 Miturbo Umwelttechnik Gmbh & Co. Kg Method of heat transformation for generating heating media with operationally necessary temperature from partly cold and partly hot heat loss of liquid-cooled internal combustion piston engines and device for executing the method

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3524327A (en) * 1968-05-31 1970-08-18 Air Liquide Method of maintaining electrical apparatus at very low temperatures
US4803958A (en) * 1987-09-08 1989-02-14 Erickson Donald C Absorption heat pumped cogeneration engine
US5581997A (en) * 1993-10-19 1996-12-10 California Energy Commission Performance enhanced gas turbine powerplants
US6484501B1 (en) * 1998-02-03 2002-11-26 Miturbo Umwelttechnik Gmbh & Co. Kg Method of heat transformation for generating heating media with operationally necessary temperature from partly cold and partly hot heat loss of liquid-cooled internal combustion piston engines and device for executing the method
US6321552B1 (en) * 1998-06-22 2001-11-27 Silentor Holding A/S Waste heat recovery system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1999766A1 (en) * 2006-03-22 2008-12-10 Seong-Hwang Rim The cooler for transformer using generation cycle
EP1999766A4 (en) * 2006-03-22 2013-01-02 Seong-Hwang Rim The cooler for transformer using generation cycle
US20080178590A1 (en) * 2007-01-29 2008-07-31 General Electric Company Integrated plant cooling system
US7716930B2 (en) * 2007-01-29 2010-05-18 General Electric Company Integrated plant cooling system
WO2012031791A1 (en) * 2010-09-08 2012-03-15 Siemens Aktiengesellschaft Method and arrangement for drying a transformer component

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